摘要
本文应用在连续性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。
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.
出处
《空气动力学学报》
CSCD
北大核心
1996年第2期234-238,共5页
Acta Aerodynamica Sinica
基金
航空基金
关键词
拟压缩性方法
近似因式分解
脱体涡
N-S方程
pseudocompressibility approach, Navier-Stokes equations,approximate factorization scheme, vortical flows.