DIAGONAL IMPLICIT MULTIGRID ALGORITHM FOR THE EULER EQUATIONS

被引:31
作者
CAUGHEY, DA
机构
[1] Cornell Univ, United States
基金
美国国家科学基金会;
关键词
Aerodynamics--Wings and Airfoils - Computer Simulation - Computers--Applications - Fluid Dynamics - Mathematical Models;
D O I
10.2514/3.9977
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A multigrid implementation of the Alternating Direction Implicit algorithm has been developed to solve the Euler equations of inviscid, compressible flow. The equations are approximated using a finite-volume spatial discretization with added dissipation provided by an adaptive blend of second and fourth differences. For computational efficiency, the equations are diagonalized by a local similarity transformation so that only a decoupled system of scalar pentadiagonal systems need be solved along each line. Results are computed for transonic flows past airfoils and include pressure distributions to verify the accuracy of the basic scheme and convergence histories to demonstrate the efficiency of the method.
引用
收藏
页码:841 / 851
页数:11
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