MULTIGRID ACCELERATION OF THE FLUX-SPLIT EULER EQUATIONS

被引：17

作者：

ANDERSON, WK ^{[1
]}

THOMAS, JL ^{[1
]}

WHITFIELD, DL ^{[1
]}

机构：

[1] MISSISSIPPI STATE UNIV,DEPT AEROSP ENGN,MISSISSIPPI STATE,MS 39762

来源：

AIAA JOURNAL | 1988年 / 26卷 / 06期

关键词：

AERODYNAMICS - Transonic - AIRCRAFT - Wings - COMPUTER PROGRAMMING - Algorithms;

D O I：

10.2514/3.9949

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Multigrid acceleration is applied to a flux-split algorithm for solving the Euler equations in three dimensions. The basic algorithm is an implicit spatially split approximate factorization method. The stability and performance of the scheme in comparison to other factorizations are examined. Results are presented for three-dimensional flows that demonstrate substantially improved convergence with the multigrid algorithm.

引用

页码：649 / 654

页数：6

共 13 条

[1]

ANDERSON WK, 1986, THESIS MISSISSIPPI S

[2]

ANDERSON WK, 1985, AIAA850122 PAP

[3] IMPLICIT FINITE-DIFFERENCE ALGORITHM FOR HYPERBOLIC SYSTEMS IN CONSERVATION-LAW FORM [J].

BEAM, RM ;

WARMING, RF .

JOURNAL OF COMPUTATIONAL PHYSICS, 1976, 22 (01) :87-110

[4]

BUNING PG, 1982, AIAA820971 PAP

[5]

JAMESON A, 1984, AIAA840093 PAP

[6]

JAMESON A, 1985, AIAA850293 PAP

[7] A MULTIPLE-GRID SCHEME FOR SOLVING THE EULER EQUATIONS [J].

NI, RH .

AIAA JOURNAL, 1982, 20 (11) :1565-1571

[8]

SCHMITT V, 1879, AGARD138 ADV REPT

[9] FLUX VECTOR SPLITTING OF THE INVISCID GAS-DYNAMIC EQUATIONS WITH APPLICATION TO FINITE-DIFFERENCE METHODS [J].

STEGER, JL ;

WARMING, RF .

JOURNAL OF COMPUTATIONAL PHYSICS, 1981, 40 (02) :263-293

[10]

STEGER JL, 1981, NASA CR3415

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