COMPRESSIBLE LAMINAR BOUNDARY-LAYERS WITH LARGE ACCELERATION AND COOLING

被引：6

作者：

BACK, LH ^{[1
]}

CUFFEL, RF ^{[1
]}

机构：

[1] CALTECH, JET PROP LAB,TECH STAFF,PASADENA,CA 91103

来源：

AIAA JOURNAL | 1976年 / 14卷 / 07期

关键词：

D O I：

10.2514/3.7170

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：968 / 971

页数：4

共 13 条

[1]

AMBROK GS, 1957, SOV PHYS-TECH PHYS, V2, P1979

[2] ACCELERATION AND COOLING EFFECTS IN LAMINAR BOUNDARY LAYERS - SUBSONIC, TRANSONIC, AND SUPERSONIC SPEEDS [J].

BACK, LH .

AIAA JOURNAL, 1970, 8 (04) :794-&

[3] FLOW COEFFICIENTS FOR SUPERSONIC NOZZLES WITH COMPARATIVELY SMALL RADIUS OF CURVATURE THROATS [J].

BACK, LH ;

CUFFEL, RF .

JOURNAL OF SPACECRAFT AND ROCKETS, 1971, 8 (02) :196-&

[4]

BACK LH, 1969, ASME J APPLIED MECHA, V36, P336

[5] INTEGRAL METHOD IN COMPRESSIBLE LAMINAR BOUNDARY LAYERS AND ITS APPLICATION [J].

CHAN, YY .

PHYSICS OF FLUIDS, 1966, 9 (02) :350-&

[6]

COHEN CB, 1956, R1294 NACA

[7]

HAYES WF, 1959, HYPERSONIC FLOW THEO, P319

[8] LAMINAR HEAT TRANSFER OVER BLUNT-NOSED BODIES AT HYPERSONIC FLIGHT SPEEDS [J].

LEES, L .

JET PROPULSION, 1956, 26 (04) :259-&

[9] EFFECT OF LARGE TEMPERATURE CHANGES (INCLUDING VISCOUS HEATING) UPON LAMINAR BOUNDARY LAYERS WITH VARIABLE FREE-STREAM VELOCITY [J].

LEVY, S .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (07) :459-474

[10] VISCOUS EFFECTS ON FLOW COEFFICIENT FOR A SUPERSONIC NOZZLE [J].

MASSIER, PF ;

BACK, LH ;

NOEL, MB ;

SAHELI, F .

AIAA JOURNAL, 1970, 8 (03) :605-&

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