DETAILED STUDY OF ATTACHED AND SEPARATED COMPRESSION CORNER FLOWFIELDS IN HIGH REYNOLDS-NUMBER SUPERSONIC-FLOW

被引：165

作者：

SETTLES, GS

FITZPATRICK, TJ

BOGDONOFF, SM

机构：

来源：

AIAA JOURNAL | 1979年 / 17卷 / 06期

关键词：

D O I：

10.2514/3.61180

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：579 / 585

页数：7

共 23 条

[1] VELOCITY PROFILES IN TURBULENT COMPRESSIBLE BOUNDARY LAYERS [J].

BARONTI, PO ;

LIBBY, PA .

AIAA JOURNAL, 1966, 4 (02) :193-&

[2]

CHAPMAN DR, 1958, NACA1356 REP

[3]

COAKLEY TJ, 1977, AIAA77692 PAP

[4]

COLES DE, 1962, R403PR RAND CORP REP

[5]

DOLLING DS, 1978, AIAA78159 PAP

[6]

GINOUX J, 1962, TN6 TCEA

[7] REYNOLDS-NUMBER EFFECTS ON SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTIONS [J].

HORSTMAN, CC ;

SETTLES, GS ;

VAS, IE ;

BOGDONOFF, SM ;

HUNG, CM .

AIAA JOURNAL, 1977, 15 (08) :1152-1158

[8] RESULTS OF A STRONG INTERACTION, WAKE-LIKE MODEL OF SUPERSONIC SEPARATED AND REATTACHING TURBULENT FLOWS [J].

HUNTER, LG ;

REEVES, BL .

AIAA JOURNAL, 1971, 9 (04) :703-&

[9]

INGER GR, 1975, AGARDCPP168 FLOW SEP

[10] APPLICATION OF TRANSFORMATION METHODS TO WEDGE-SHOCK/BOUNDARY-LAYER INTERACTIONS [J].

KOTANSKY, DR .

AIAA JOURNAL, 1971, 9 (04) :731-&

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