LAMINARIZATION OF A TURBULENT BOUNDARY LAYER IN NOZZLE FLOW

被引：12

作者：

BACK, LH

CUFFEL, RF

MASSIER, PF

机构：

[1] Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA

来源：

AIAA JOURNAL | 1969年 / 7卷 / 04期

关键词：

D O I：

10.2514/3.5196

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：730 / &

共 14 条

[1]

Back L.H., 1964, INT J HEAT MASS TRAN, V7, P549, DOI [10.1016/0017-9310(64)90052-3, DOI 10.1016/0017-9310(64)90052-3]

[2] 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-&

[3] FLOW PHENOMENA AND CONVECTIVE HEAT TRANSFER IN A CONICAL SUPERSONIC NOZZLE [J].

BACK, LH ;

MASSIER, PF ;

CUFFEL, RF .

JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (08) :1040-&

[4]

BACK LH, 1967, P HEAT TRANSFER FLUI, P410

[5] THE LAW OF THE WAKE IN THE TURBULENT BOUNDARY LAYER [J].

COLES, D .

JOURNAL OF FLUID MECHANICS, 1956, 1 (02) :191-226

[6]

CRABTREE LF, 1963, LAMINAR BOUNDARY LAY, P427

[7]

Hartree DR, 1937, P CAMB PHILOS SOC, V33, P223

[8]

KLINE SJ, 1967, FLUID MECHANICS INTE

[9]

LAUNDER BE, 1964, 77 MASS I TECHN GAS

[10]

Moretti P.M., 1965, Int. J. Heat Mass Transfer, V8, P1187, DOI DOI 10.1016/0017-9310(65)90062-1

← 1 2 →