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

隐式格式求解拟压缩性非定常不可压Navier-Stokes方程
引用本文:白鹏,崔尔杰,周伟江,李锋.隐式格式求解拟压缩性非定常不可压Navier-Stokes方程[J].计算物理,2005,22(5):386-392.
作者姓名:白鹏  崔尔杰  周伟江  李锋
作者单位:中国航天空气动力技术研究院,北京,100074;中国航天空气动力技术研究院,北京,100074;中国航天空气动力技术研究院,北京,100074;中国航天空气动力技术研究院,北京,100074
摘    要:采用Rogers发展的双时间步拟压缩方法,数值求解不可压非定常问题.数值通量分别采用三阶精度Roe格式和二阶精度Harten-Yee的TVD格式离散.为了加快收敛,提高求解效率,试验了几种隐式格式(ADI-LU,LGS,LU-SGS).针对经典的低雷诺数(Re=200)圆柱绕流问题,比较了不同隐式方法的计算结果和求解效率,以及两种数值离散格式计算结果的异同.最后采用Roe格式数值求解了两种典型的低速非定常流动问题:绕转动圆柱(ω=1)低雷诺数流动;NACA0015翼型等速拉起数值模拟.

关 键 词:隐式格式  低雷诺数  拟压缩方法  不可压方程
文章编号:1001-246X(2005)05-0386-07
收稿时间:2004-05-20
修稿时间:2004-10-29

An Implicit Method for the Pseudo-Compressibility Incompressible Navier-Stokes Equation
BAI Peng,CUI Er-jie,ZHOU Wei-jiang,LI Feng.An Implicit Method for the Pseudo-Compressibility Incompressible Navier-Stokes Equation[J].Chinese Journal of Computational Physics,2005,22(5):386-392.
Authors:BAI Peng  CUI Er-jie  ZHOU Wei-jiang  LI Feng
Institution:China Academy of Aerospace Aerodynamics, Beijing 100074, China
Abstract:A pseudo-compressibility method developed by Rogers is used to solve the incompressible Navier-Stokes equation. Numerical flux is scattered through 3rd order Roe scheme and the 2nd order Harten-Yee TVD scheme separately. In order to accelerate convergence, several implicit methods(ADI-LU, LGS, LU-SGS) are accepted. Efficiency of different methods are shown as a classical flowfield around a cylinder in low Re(Re=200). Roe scheme is used to simulate two low speed unsteady problems:Low Re flowfield around a rotational cylinder(ω=1) and flowfield around a pitching NACA0015 airfoil with identical pitching rate.
Keywords:implicit scheme  low Re  pseudo-compressibility method  incompressible Navier-Stokes equations
本文献已被 CNKI 维普 万方数据 等数据库收录!
点击此处可从《计算物理》浏览原始摘要信息
点击此处可从《计算物理》下载免费的PDF全文
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