摘要
In this paper, the implicit approximate factorization schemes is combined with themultigrid method for computing the transonic flow fields of A-27 inlet. The numericalresults have shown that the multigrid method based on the approximate factorizationschemes can eliminate numerical vibration, simplify parametric choice and accelerateconvergent rate.
In this paper, the implicit approximate factorization schemes is combined with themultigrid method for computing the transonic flow fields of A-27 inlet. The numericalresults have shown that the multigrid method based on the approximate factorizationschemes can eliminate numerical vibration, simplify parametric choice and accelerateconvergent rate.
出处
《数值计算与计算机应用》
CSCD
北大核心
1999年第4期283-292,共10页
Journal on Numerical Methods and Computer Applications
基金
航空科学基金
