GASEOUS FILM COOLING AT VARIOUS DEGREES OF HOT-GAS ACCELERATION AND TURBULENCE LEVELS

被引：25

作者：

CARLSON, LW

TALMOR, E

机构：

来源：

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER | 1968年 / 11卷 / 11期

关键词：

D O I：

10.1016/0017-9310(68)90048-3

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

引用

页码：1695 / +

页数：1

共 31 条

[1] SOME OBSERVATIONS ON REDUCTION OF TURBULENT BOUNDARY-LAYER HEAT TRANSFER IN NOZZLES [J].

BACK, LH ;

MASSIER, PF ;

CUFFEL, RF .

AIAA JOURNAL, 1966, 4 (12) :2226-&

[2]

BECKWITH IE, 1961, R104 NASA TR

[3] TOTAL BOUNDARY-LAYER MASS FLOW WITH MASS TRANSFER AT WALL [J].

CHAPMAN, GT .

AIAA JOURNAL, 1966, 4 (09) :1688-&

[4]

COMTEBELLOT G, 1966, J FLUID MECH, V25, P667

[5] FILM COOLING WITH HELIUM INJECTION INTO AN INCOMPRESSIBLE AIR FLOW [J].

GOLDSTEIN, RJ ;

RASK, RB ;

ECKERT, ERG .

INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1966, 9 (12) :1341-+

[6] FILM-COOLING EFFECTIVENESS WITH INJECTION THROUGH A POROUS SECTION [J].

GOLDSTEIN, RJ ;

SHAVIT, G ;

CHEN, TS .

JOURNAL OF HEAT TRANSFER, 1965, 87 (03) :353-+

[7]

Hartnett J., 1961, ASME J HEAT TRANSFER, V83, P293, DOI [10.1115/1.3682263, DOI 10.1115/1.3682263]

[8]

Hartnett J. P., 1961, INT DEV HEAT TRANSFE, P682

[9]

HATCH JE, 1959, D130 NASA TN

[10] EXPERIMENTAL METHOD OF MEASURING INTENSITY OF TURBULENCE IN A ROCKET CHAMBER [J].

HERSCH, M .

ARS JOURNAL, 1961, 31 (01) :39-45

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