SHOCK-FITTING APPLIED TO RELAXATION SOLUTIONS OF TRANSONIC SMALL-DISTURBANCE EQUATIONS

被引：10

作者：

HAFEZ, MM ^{[1
]}

CHENG, HK ^{[1
]}

机构：

[1] UNIV SO CALIF,DEPT AEROSP ENGN,LOS ANGELES,CA 90007

来源：

关键词：

D O I：

10.2514/3.60711

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：786 / 793

页数：8

共 16 条

[1] ACKERET J, 1947, TM1113 NACA
[2] BARNWELL RW, 1967, R268 NASA TR
[3] MODERN DEVELOPMENTS IN TRANSONIC FLOW
COLE, JD
[J]. SIAM JOURNAL ON APPLIED MATHEMATICS, 1975, 29 (04) : 763 - 787
[4] FERRARI C, 1968, TRANSONIC AERODYNAMI
[5] GROSSMAN B, 1970, AIAA701322 PAP
[6] CONVERGENCE ACCELERATION OF RELAXATION SOLUTIONS FOR TRANSONIC FLOW COMPUTATIONS
HAFEZ, MM
CHENG, HK
[J]. AIAA JOURNAL, 1977, 15 (03) : 329 - 336
[7] HAFEZ MM, 1975, USCAE132 SCH ENG REP
[8] JAMESON A, 1975, 2ND P AIAA COMP FLUI, P148
[9] MAGNUS RM, 1973, TN73SPO3
[10] FAST SEMIDIRECT METHOD FOR COMPUTING TRANSONIC AERODYNAMIC FLOWS
MARTIN, ED
[J]. AIAA JOURNAL, 1976, 14 (07) : 914 - 922