NUMERICAL COMPUTATIONS OF 2-DIMENSIONAL VISCOUS BLUNT BODY FLOWS WITH AN IMPINGING SHOCK

被引：36

作者：

TANNEHILL, JC

HOLST, TL

RAKICH, JV

机构：

[1] IOWA STATE UNIV,DEPT AEROSP ENGN,AMES,IA 50010

[2] IOWA STATE UNIV,ENGN RES LAB,AMES,IA 50010

[3] NASA AMES RES CTR,MOFFETT FIELD,CA

来源：

AIAA JOURNAL | 1976年 / 14卷 / 02期

关键词：

D O I：

10.2514/3.61358

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：204 / 211

页数：8

共 21 条

[1]

BECKWITH IE, 1961, D625 TN NASA

[2]

BERTIN JJ, 1975, J SPACECRAFT ROCKETS, V12, P155

[3] SHOCK-WAVE SHAPES AROUND SPHERICAL-AND CYLINDRRICAL-NOSED BODIES [J].

BILLIG, FS .

JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (06) :822-&

[4] SIMPLE TECHNIQUE FOR PREDICTING TYPE-III AND IV SHOCK INTERFERENCE [J].

BRAMLETTE, TT .

AIAA JOURNAL, 1974, 12 (08) :1151-1152

[5]

Edney B., 1968, FFA115 AER RES I SWE

[6] SHOCK INTERFERENCE HEATING IN HYPERSONIC FLOWS [J].

HAINS, FD ;

KEYES, JW .

AIAA JOURNAL, 1972, 10 (11) :1441-&

[7]

HOLST TL, 1975, MAR NASA C AER AN RE

[8]

HOLST TL, SP347 NASA

[9]

KEYES JW, 1973, D7139 TN NASA

[10] MULTISHOCKED, 3-DIMENSIONAL SUPERSONIC FLOWFIELDS WITH REAL GAS EFFECTS [J].

KUTLER, P ;

REINHARDT, WA ;

WARMING, RF .

AIAA JOURNAL, 1973, 11 (05) :657-664

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