A PARTIALLY IMPLICIT METHOD FOR SIMULATING VISCOUS AEROFOIL FLOWS

被引：5

作者：

BADCOCK, KJ

机构：

[1] Aerospace Engineering Department, University of Glasgow, Glasgow

来源：

INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS | 1994年 / 19卷 / 03期

关键词：

NAVIER-STOKES; PARALLEL; PARTIALLY IMPLICIT;

D O I：

10.1002/fld.1650190305

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

A partially implicit method for the unsteady compressible Navier-Stokes equations is developed. The method is based on an explicit treatment of streamwise fluxes and an implicit treatment of normal fluxes. This leads to a linear system which is generated by an efficient finite difference procedure and which is block pentadiagonal. The method is tested on a shock-induced oscillatory flow over an aerofoil. Parallel implementations of an explicit, fully implicit and partially implicit method are investigated.

引用

页码：259 / 268

页数：10

共 12 条

[1]

BADCOCK KJ, 1993, GU9313 AER TECH REP

[2]

BADCOCK KJ, 1993, GU9323 AER TECH REP

[3] IMPLICIT FACTORED SCHEME FOR COMPRESSIBLE NAVIER-STOKES EQUATIONS [J].