HYPERSONIC TRANSITIONAL BOUNDARY-LAYERS

被引：12

作者：

OWEN, FK

HORSTMAN, CC

机构：

来源：

AIAA JOURNAL | 1972年 / 10卷 / 06期

关键词：

D O I：

10.2514/3.50209

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：769 / +

共 13 条

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[2]

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[4] STRUCTURE OF TURBULENT BOUNDARY LAYERS [J].

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REYNOLDS, WC ;

SCHRAUB, FA ;

RUNSTADLER, PW .

JOURNAL OF FLUID MECHANICS, 1967, 30 :741-+

[5] AERODYNAMIC NOISE IN SUPERSONIC WIND TUNNELS [J].

LAUFER, J .

JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (09) :685-692

[6] SOME STATISTICAL PROPERTIES OF THE PRESSURE FIELD RADIATED BY A TURBULENT BOUNDARY LAYER [J].

LAUFER, J .

PHYSICS OF FLUIDS, 1964, 7 (08) :1191-1197

[7]

LAUFER J, 1968, SP216 NASA, P1

[8] UNUSUAL BOUNDARY-LAYER TRANSITION RESULTS ON CONES IN HYPERSONIC FLOW [J].

MATEER, GG ;

LARSON, HK .

AIAA JOURNAL, 1969, 7 (04) :660-&

[9]

Morkovin MV., 1959, J APPL MECH, V26, P319, DOI [10.1115/1.4012040, DOI 10.1115/1.4012040]

[10] TRANSITION EXPERIMENTS ON A FLAT PLATE AT SUBSONIC AND SUPERSONIC SPEEDS [J].

OWEN, FK .

AIAA JOURNAL, 1970, 8 (03) :518-&

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