SUPERSONIC TURBULENT BOUNDARY-LAYER IN ADVERSE PRESSURE-GRADIENT .2. DATA-ANALYSIS

被引：21

作者：

STUREK, WB

DANBERG, JE

机构：

来源：

AIAA JOURNAL | 1972年 / 10卷 / 05期

关键词：

D O I：

10.2514/3.50167

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：630 / &

共 13 条

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

BARONTI, PO ;

LIBBY, PA .

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

[2]

COLES D, 1953, 2071 JET PROP LAB RE

[3] AN EXPERIMENTAL INVESTIGATION OF HYPERSONIC TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENT [J].

HOYDYSH, WG ;

ZAKKAY, V .

AIAA JOURNAL, 1969, 7 (01) :105-&

[4]

KEPLER CE, 1962, TDR6287 ASD AIR FORC

[5]

KRISTLER AL, 1958, BRLR1052 BALL RES LA

[6]

MCLAFFERTY GH, 1962, J AEROSP SCI, V29, P1

[7] EXPERIMENTAL INVESTIGATIONS OF COMPRESSIBLE TURBULENT BOUNDARY LAYER AT VERY HIGH REYNOLDS NUMBERS [J].

MOORE, DR ;

HARKNESS, J .

AIAA JOURNAL, 1965, 3 (04) :631-&

[8] THE DRAG OF A COMPRESSIBLE TURBULENT BOUNDARY LAYER ON A SMOOTH FLAT PLATE WITH AND WITHOUT HEAT TRANSFER [J].

SPALDING, DB ;

CHI, SW .

JOURNAL OF FLUID MECHANICS, 1964, 18 (01) :117-143

[9]

STALMACH CJ, 1958, DRL410 U TEX DEF RES

[10] SUPERSONIC TURBULENT BOUNDARY-LAYER IN ADVERSE PRESSURE-GRADIENT .1. EXPERIMENT [J].

STUREK, WB ;

DANBERG, JE .

AIAA JOURNAL, 1972, 10 (04) :475-&

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