首页 | 本学科首页   官方微博 | 高级检索  
     

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
Affiliation: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.
本文献已被 CNKI 维普 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号