首页 | 本学科首页   官方微博 | 高级检索  
     检索      

几何微扰动对脱体涡非对称性影响的数值分析
引用本文:蔡晋生,贾剑波.几何微扰动对脱体涡非对称性影响的数值分析[J].空气动力学学报,1997,15(2):211-215.
作者姓名:蔡晋生  贾剑波
作者单位:[1]西北工业大学 [2]北京航空航天大学
摘    要:利用拟压缩性方法,Beam-Warming近似因式分解格式数值求解三维定常不可压缩Navier-Stokes方程采用Degani-Schiff修正的Baldwin-Lomax代数湍流模型,计算了绕尖头正切拱型旋成柱体的大迎角大雷诺数脱体涡流场,计算结果表明,在柱体头部施加微小的非对称几何扰动时,可以得到与实验相符的非对称脱体涡。

关 键 词:拟压缩性法  几何扰动  非对称脱体涡  N-S方程

Numerical Simulation of the Effect of Geometrical Disturbances on Vortex Asymmetry
Cai Jinsheng.Numerical Simulation of the Effect of Geometrical Disturbances on Vortex Asymmetry[J].Acta Aerodynamica Sinica,1997,15(2):211-215.
Authors:Cai Jinsheng
Abstract:The method of pseudocompressibility was used in solving the three-dimensional steady incompressible Navier-Stokes flows. The solution procedure cmploys the Beam-Warming implicit approximate factorization scheme. The Baldwin-Lomax algebraic turbulent model together with the Degani-Schiff modification was used for Keynolds -averaged Navier -Stokes cquations to numerically simulate high-incidence high Reynolds number vortical flow about a tangent-ogivc cylinder. To reproduce the experimentally observed asymmetric vortices, it was found cssential to introduce a small asymmetric geometrical disturbance near the body apcx.
Keywords:method of pseudocompressibility  gcometrical disturbance  asymmetric vortex  
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